5
& 87
* 97 #
- 7/ 5 6'()
* +,- ." / * 0 * .1 2-)3-
4) 5
&
; <* 5 6 *-/):
.
. /0 .
1 23 .
6
> 9 = < 9 7:8 ;3 5-
4 7
8 +
+ ,-
6
4 7
8
47 =- 0 4
*
>
?# 0
@
"
47
81
.
4 5-
348-339 "#$ 1396
4
B
F M 4 N2 O
+/ L 4 I J
K 3 H ;3 + / 3 8 +0 4 F 0 . 4 D E 3 > 3 6 A B . C 3 ; : ? @
10 6 3
S
L4
3 ?@ I J .
4 3
8 :4
F 0R 0 M4 36
; P : Q
. 4
X ; 0
)8 D YV
( 8.
3 V W3 J F)8 + /
F ( ;8 3 , U 3 ? @ U . 4 F 4 3
Q ; > [:/ . 3
Q ; . C+ 4
L4 4>
2Z Q ; 3
/
.+ / L 4 : + 3 N2 O XZ
3
+ 8 9 XE
3X
? L ^JD . F
3 03 ^ 4
@>
8
3 > 3 0 ] L 4 - ; \L 3
L4
L 4 Z 67 4 3
2Z
. / 03 ` @
L 4 Z 54 L 4 X9 @ 6
L4
3>3 0 ] / S
5 MF = F . ;
L 4 Q ; 3. 4
L 4 Z 68 . ` @ Z 26 L 4 X9 @ 10
L 4+ 3
@ . F3
, .
> 3 3 F :
0 F C+/ 3 8= c 3
L4 .
>30
0 F C+/ 3 8= c Q ;
. 3
Q;
L 4Q ; 3 0 F C+/ 3 8= c
8
.
8 :4
F 0R
MF . C H ;3 + / 3 8 +0 4
F
3>3
:5
D 5 6 C-7
Large Eddy Simulation of flow around a Horizontal-axis wind Turbine at Different
Rotational Speed
A. A. Veisi
Department of Mechanical Engineering Sistan and Baluchestan University, Zahedan, Iran
M. H.ShafieiMayam
Department of Mechanical Engineering,Bozorgmehr-University of Qaenat, Qaen, Iran
Abstract
The present study focuses on the flow around a horizontal axis wind turbine. Large Eddy Simulation has been employed in order to
study the flow at different rotational speeds. Anisotropic residual stress tensor is driven by The Smagorinsky model. Three
simulations were performed at different tip speed ratio of 3, 6 and 10. The acquired results are in good agreement with presented
experimental data in literatures. It is also revealed that development of the wake is decreased when downstream velocity is increased
along the horizontal line at different downstream distance of wind turbine. In addition, velocity defect behind the wind turbine is
increased when tip speed ratio increases but the recovery of wake is happened faster. At rotational speed equals 6, minimum velocity
is 54% of the initial velocity and maximum efficiency is 67% at the lateral section of wind tunnel where the tip of blade is located,
while they are 26% and 68% respectively when rotational speed is 10. Turbulence intensity is increased by increasing Tip Speed
Ratio while separated vortices from the blade are disappeared later. The effect of separated vortices from the blades of wind turbine
are not seen when rotational speed is 3, while they are revealed at rotational speed of 6 and 10. As a result, it can be concluded that
the effect of separated vortices are augmented when rotational speed is increased.
Keywords :Wind turbine, large eddy simulation, turbulence flow, Smagorinsky subgrid-scale model.
+/
- 1
( 8
n7 . F / V 4 >
2:L .
73 Q n/ 3 = c . X9 @ + 3 3 > 3
5 MF + / V 4 .
; 3 :/ + 3 L ; 6
3>3
2
5 V X:E 3
5 MF = F ^ 0 o 3
> DDE C
i ? > .[2] )8
c 4 > + /> 3
73 S ^9
. 4
8 9 F)8 /
RB + 0
+ 3 + /> 3 + . C
2:L E 0
3 Q
= 9
F3 F
4 > + /> 3
73 . 1
+ -1
+d
0 -3 2V
4 4
M 4 X3 9 3 +d
e
+d + ? D Q ;
2L 3 > 0 .[1] 4 . 7C
f
4 4 + 3i ;
3 + /> 3 ^ 4 I4
V + /R 4
3 >3 6 0
)8 3 . C . 4
8 9 C
0 X9. C 3
+ - 3 5 MF
: L4 ( 4> )
F mf + /> 3
= 9
\L 3
( 4 l 3) 3 > 3
1
Wake
Turbulence Intensity
2
*
shafiei@buqaen.ac.ir :
95/02/01 :
!
95/06/01 :( ) !
5/ ( 5
&
-2
>D @ 9H/ ? -1-2
+ I3 4 + /
@ H ;3 + / 3 8 +0 4 F (
D +/ @ = c
F X@ n D
B 3 H ;3
+/ V4
: nD
+ L (
. F R 61
4E
;/ K 0 . F X@ A 8
D
5 MF
5
(
0
+ /Q R > 3 H ;3 + / 3 8 +0 4 F
( .
C 3 X
8
9 nD
+ L +0 4 F
+ 3. F3 (
> +/
E H ;3 + / 3 8 +0 4 F
0
L mI 3 n D
+ L (
4E
;/ R `
> 1 A Z DNS
4E
;/ `
3
Q;
.[13] F
t +/ @
S E QO3 0 2 B 3 ? @ I J
4E
E
p
5 4 =l I 3 c QO3 . 4 F X - 3 c
: 4 0= Z 3 ) n . C+ 3 F+ 8 2
( 1)
=0
+
.
=
−
1
( 2)
;, . 4 F 2
- .
(x, t) ( 2)
I
0 + 8Y4
H ;3 + / 3 8 +0 4 F (
L4
: 4 F
. - (4) (3) =l I
m
3 L 4.
= +
( 3)
〈
〉
=
+
( 4)
F+ 8 2
L4.
+ KE L 4 .
. F3
4
L 4.
:
L 4.
F
A B . C +0 4
3> 3
E
I4 Q 5 = L 3 . 4 3 > : X9 @ 3 /.
73 Q n/ 3 = c .
: + 3 + 3 + /> 3 + /
. 4 + 3 i ; @ B n7
I 6 + 3>3
2:L .
MF
4 3 K 3
/ 5- 0 + L = I J
R @ > 3 [3 ] 4 F p , D E 3 > 3 6 4 >
q3
I 3>3
4 / X +0 4 F Q
:L Q 1
0 ?@
K > 3
F3
MF . C > [:/ .
1
. 4 F M 4 H ;3 + / 3 8 +0 4 F (
3
2
>3 0
>3 6 ;
: 9
3
@
3 3 3 1 > 3 XZ @ > 3 6 ;
@ . 4 Fn D
@
: 9> 4 >
@ + 3>3
J9
. [4 ] F N I + 3 > 3 0
+
3 3 L 4 = r 4 3 3 [5]. :/
:/
Q:
8 ;3 + / 3 8 +0 4 F ( 0 M 4 7
( 8
>3 6 ;
@
/ - /. . V . ;r
F
, > 3 + / Y4 +
[
+/ 3 8 3
@
F
@
5 MF + / V 4 >
O . F 6 M + 61 + / 3 8 3 > 3 0
3 H ;3 + / 3 8 +0 4 F ( 0 M 4 3 [6]. :/ X8
V + 3i ;
3>3 0
)8 + M : +0
l IJ
+ /> 3
3 4 l 3 + /> 3 0 XZ @
Q :/ 3
Q; + 3
/.
U .
4 3
4>
9 M4
+ 3 + /> 3
:L Q ;
3 + /> 3
/ 03
L; RB
4 n/ = c 4 3 3[7]. :/ . 4 . 8
0
; +
= 9 ` @ 3 3 4 + 3
.- + 3
+ 3 i ;
+ 3 + /> 3
, JF + 3
0
M4 3
3 D E 3 > 3 6 R @ . C [8] . :/
. F3 :
DES RANS
3+
3. C= M +/ L 4
> +/ L 4
. - /. = I J .
9 IJ
/
<
+ 3 - U DES RANS R
/ 3. C
Q :
V + 3 DES 3 . C +l 3 + / L 4
. 3. /
.3 > 3 +/ 0 F C +/ 3 8
R 6
+ / fO- / 5- 0 I J 6
[9] . :/
4 . V 1 3 > 3 6 XO2O . V 1 P 3 > 3
F 4
. - /. .
9 IJ
N2 O 5 MF = F
3
4>
XO2O . V 1 P F 4 R
[10] . :/ s . .
3Q
4
3 3>3
C +/ 3 8 [
@
. - / 5- 0 I J
3 > 3 + / QV 1 3
I
7C / 0 F
. - PIV / 5- 0 ( 0 M 4 3 [11] . :/ s d.
+ / 3 8 = Z fV 3 + 3 > 3 6 ;
@
F 5:/
V
P > 3 +/ 0 F C [
3 [12] . :/
< . F
V F MF . C + / fO-
... + / L 4 3 D
.- 3 X 3+
3 . C 5 MF = F I J
. F
3 03 ^ 4
7 @ l 3 5 MF = F
+ L +0 4R 0
M4 3
8 = Z =I J ` .
4
/ >
. 4 F p , Y4 : L
+ 3 R 4. C
. :
4 3. C.
Y4 = LtB YD
.
K 7e L 4 .
+ KE = LtB . C 6
>3 6 A B . C.
X
IJ 3
F I4 ? @
3 tL > :/ 0 . F V N2 O
+/ L 4 E 3
c
5 MF + / V 4 / 3 8 - m ?
L 4 + /.
3. 8 / V 9 4 3 IJ
; >3
2:L 3 7
3
+/ L 4= c 4 3
L4 r 3 5 = L
. F / V IJ >3
2:L 3 . C .
c . C.
L; 6
/> 3 . 1 utZ
?@
U
) . 8 9 M4
i ; >
2:L Q ; > [:/ + 3
+ / +d i ?
:/
F
=E ? 3
L 3
. 3 / V M + 3
I J 6 ?@
1
4
Reynolds-Averaged-Navier-Stokes (RANS)
5
Reynolds Stress Models
Large Eddy Simulation (LES)
Near wake
3
Far wake
2
340
>
@ :E
I Mn
B
D ℓD F 3
fO- F 2 Q y S ,
8 :4 3 c W B 0
4
8 :4
3 m4 CD
fE 2x X@ + 3 ; + 5 + /R . F ∆ 2 z L
d . 4
F 7 - H ;3 + / 3 8 +0 4 F (
^3
0 M4 3
<
R [15]. :/
3 @tZ I3
.
< CD 0 m4
2E
D 6 2
. 8 = Z [17]. :/
[16] 2 Y4 R > +
St
[18]. :/
3 Y4 ; + 5 + /R
5
8 :4 R 0
/R > F 7 - [19]. :/
+ /R /. 3 @tJZ
4 5 + /R 3
M8 3
3 C 3
4 3 , 3c 6
8 :4 3 c .. F
IJ >
. F vO
29+ F 3 ,
2x Y F
D3 J
4 F v O C D = 0/ 1 3 3
8 :4 3 c D
K
F 0
3 3 2 z L. 4 F 3, U 3 3V
: F
4 E 0 J3 0
4 F
8
7/
(17)
∆= H∆@ ∆I ∆J K
+,- ." / * 0 * .1 9 JKL -3-2
Y4
F3 1
t3 / 5- 0 U
4 3 IJ >
.. 4 F @ B d
+ t 2011 R 4 [20] |
- NRELS826 i 0 3 > 3 + /
F M4 X
F3l3 3m ?
4 F @ B+ 8 3X
> . F3
3
+ 3 > [:/
F 3 F + 30 3 :
4 @
3 :/ X
0 2 N Z .[21] F 3 m4
:
O4
Y4 l 3 0
L 3
/. C + 3
3 m ?
. 4 F < [22] 4
F 2 +/ L 4v ? 3
F 2 v?
> 3 At V .
= M ] 4
=l I 3 (2) J3
: F N I 0= Z 3
4 : Q
, 0
= M
>
=
−
( 5)
4
9 X3 9 0
Q
3
>
〈
〉=〈
〉 − 〈 〉〈 〉
( 6)
P : Q
N I (2) J3
(3) J3 + )5 C 3
0 = Z 3 F utZ F 2 - 6
;
=
- ! δ#$
( 7)
2
( 8)
= +
!
3
+
3
'
()
wO- ((()
*+ .
& 7 5 ) M4-)
-4-2
iM
zL RBm
3 IJ >
F +0 4 F 3 X
F mf 3 X ;
3 > 3 . 1/8 m 2/7m،11/14m
J9 ,
D . 4 5D 3 3 3 X +
0 >3
2Z . 4
4 0/817 mm > 0 }J4 0
; iM . 4 > 3
:L + /Q 1 0
F F 3
B. :/ .(1 X F)
3 >3
4 / X +0 4 F + 3 + /> 3 +0 4 F
4 / IJ >
. F3 . C.
> [:/ q 3
X F
E . 4 F C / 5- 0 R
3- D 9 3 > 3
3 c S E QO3
0 2 B 3 ?@ I J
4E
. 4 FX -
46
−
7
( 9)
7
+ 2. (v
()0 (v))'
() 1 v
() = − 29 + 2 (()
v
(13)
8
:̅ =
-2-2
7 =>?
<
=@A
+
=>A
=@?
B
(15)
m ?. F Y
4 : +/
Q
F 2 y 3
@ + 3 8 C; l 3 J3
0
C; . 4 F 2 Q
: F R
0 = Z 3 2 Bt V R B ?
9 3+ 3 8
= (CD ∆) :̅
1
341
I
0
=l I ( 3 - ; H ;3 + / 3 8 +0 4 F (
+ /Q
X - > X@ + 3 .
C 1 fE 2x
Q =l I W B0
5 MF C; + /R 0 M 4 3 0
+ / 3 8 +0 4 F (
fE 2x .
4 30
- 4 . F X@ 6
; : Q
. R 3 H ;3
R >
. 4 F 7 - [14]
8 :4 Y4 R >
JV + 3 8 C; R 0 M 4 3 3
̅
= −2 :
(14)
)O @ ?P Q / 0 * .1 5) : -)R N" -1 N
Mixed models
−
0= Z 3p
& )4 I
= ℓD : ̅
3
=
1
3c+ 0 L 4 / S E =f O n 4
36 3S E n 4; .
> 4YE
] 4 ,̂
3 7C QV 1 E . 4 F
(() = ω,̂
ω
(10)
wO- *) .
3 3SE YE ;
3
I9
S E Y E 3 > 4 Y E 0 0 J3 3 R 4 L 4 . F
: F X
()0 = v
v
() − ω
(() 1 *)
(11)
v
() 4 (S E Y E
L 4)
L 4 (v)0 (11) J3
. 4 + 0 L 4ω
(() (> 4 Y E
L 4) W2J
L4
0= Z 3S E =f O n 4 p
5 4 =l I
: F
03
2. (v)0 = 0
(12)
45
()
1& "
:
2
:
Q
( , ) m4
y
:̅
(16)
Closure problem
Mixing-length hypothesis
341
. 4>3
+/
QV 1 C 7/5 R I
)O @ D
4E
&
D
4
F
C[ m ?
1100000
0/3965
2700000
0/4095
3400000
0/4102
5/ ( N@
'"$ -3
F
D 3, U
3 C[ m ? X@ EZ 4 3 7C
+ 4
F I3 3 L 4 X
(5 4) + /X F .(3 X F) 4
+ 3 3 > 3 QV 1 ; 0
)8 D YV
. C
.3 > 3 0 ] 5D 1D 2Z
6 S
L4
8 = Z +0 4R
3, U
3 ?@
U . /
D [20]
Y4
F p , +0 4 F [20]> / Y4
U
4 3 U
> 3 .(5
4 + /X F) 4
F
> 3 0 ] 5D 2Z
7
C 3 V W3 J / 5- 0
= tV
I J
Q IJ
75 q 3 = c 3
. 4 Fn
75 q 3 = c / 5- 0 U
F
L4 >
A E
. 4 10 m/s
3 X
+
3
F
A B . C +0 4
L4
= Z 3 5 MF = F . 4 TI =%0/3 5 MF = F
: F
〈u 〉7/
TI =
U0QR
λ = ΩU/
VW
L4
N I ^C
L4 3
I
(18)
(;r p L € F 3
;
4 F < 0 J3
3 X +/
S
L4
i IF U
VW
=10 λ2=6 λ1=3
S
4 3 2E 0
.0/3924
1800000
3> 3
1 & " /7 " -2N
+
^C
- IT+ - -1I7
F 0
Fn
4 6 3
4 6 X F S E QO3
8 9
4 .
3> 3 +/
4 0 @ >
D3
3 c QO3 . 4 F n/ QO3 >
/ QV 1 .
6
0 M4 X
3 .(2X F) F X F
3 X +~
S - C 6 MRF R AtV 3 S E QO3 + 3 1. ;r Q
- F ( > W 9 . ;r Q 6
. 4 FvO + l
0 M4
F3
8 1 S E + /QO3 + 3 . C +0 4
. 3 l3
4E
;/ ( >
E
E n,@ ( 0 =l I +0 4
8 + 3 Q/ o >
4 3 SIMPLE n 5 W B 0 - p . 4 F M 4
+ I3 2@
3Q
3 SIMPLE (
X? M +
3 p
I
+0 4
8 . F utZ
+0 4
8
4
4 +
3 I
+;
V4 + 3 F . F3
:? p
0 =l I
0
F; + @ 3+ 3 F. 4 F M4 K
4 /+ 3
+ / 3 8 +0 4 F (
. F F 0 XD
/v C
4
L4.
F vO + F 3 3
4E
F H ;3
. F 3 F (DNS 3
) F
F (x, t) F 2
D1 / > 0 . 4 m4
2 zL 3
4E
F 2Z
X@ + - 3 +d X F + /
@ F3 ;
4E
F
+d 0 7C X3 9
F
F vO 3 . F
3 = F 3 +0 4 F F \L 3
93 : +/ @
3 +0 4R
N2 O
4 E + / F + 3 c[ m ? . F
r /
.- U > 3
D .(1 R C) 4 F 4 3
C . 2 2/7 0 ;
4E
F + 3 c[ m ?
1
v O ? @ I J + 3 . 2 2/7
4E
F > 0 .
@ 3 €3
4E
F 0 . 2 0/4
@ . 4 F
-/
6
. 4 3c @ 3 € 3
D3
SE
+ 3
4 E . 0 2/1GHz (0 = 9 3 cpu 6 3 + /
vO
Z 3
0 p 8 . 4 L 4 160
@ +0 4 F /
4E
... + / L 4 3 D
N@ 87 -5-2
L4
q3
u J4
. 4 F R :L
(19)
L 4Ω ,
4+ 3 ?@
L. 4
8 = Z +0 4
6#[
4 ReZ =105 3
. 4
F λ3
6 3
D
3 λ2 = 6 + 3
. 4 61
6 0
L > I9
D
3 7C X3 9 = c
4 30
L
F • 3
+
= 9 - 3R` + 3.
3 > 3 + 2:L + / fO0 : 2V.
+ : 0
L
+ 3>3 + 3
R @ > 3 .[23] 4 l 3 0
L 3 3 >3
+/ V4
+/ 3 8
7 - [24]. 4 M
0
L 0 XD
3 D >3
@
MF . C
3>3
6#[
C V = 9 +d
p
+ D3 . 9
4 3. F 3 ReZ
8 ;3 L 4 At V . 4 L 4 At V mI 3 m4
>3
. 4 3 > 3 Y4
3. C0 -3
= 9 / .c[ m ? 3 + /> 3
@ B 3 )8 c X L 0
> 0
+d +d X 3 3 0 F
4 +d
4
: 4 F < 0 J3
m ?> . 4 3
c[ = 7
1
+A
(20)
Sliding mesh technique
342
>
F (
. 4
0 [20]
M4
V4
< P [ 7 \"* -4
n
I M-
@ :E
Q 0 + 3 H ;3 + / 3 8 +0 4
. 4
3>3
'() N ,7) -1-4
>3 0 ]
X ;
F ,
( 8 X@ 4 0 . :B 0 ]
D YV
N2 O
+/ L 4 + 3 3
L 4 Q ; . 4 F 4 3 N2 O XZ
3
; / 5- 0 U
3>3
4>
3X
?L
. 3 l 3 B O3 F / Q ; > ^9
. 42
3 > 3 Y4
Fv C @
7C 3 L 4
F
4 /+ 3 ,
F3
3X
?L @
3
8 = Z =I J
1 / . 4 Z 12/1
>
3 [25]
: 73 X + 3
Z 10 +l 3
. 4 F
8
R > . 8 0 4 Y4 i ? > R @>
( 8 6) + / X F
L 4 I3 3 X
F + 8Y4 U
/- 3. 4 F
. - 10 6 3 S
L4
+ 3
+ E M ‚ ? L ^B D
8 wOL 4 ^0
> . 3
Q/ + K@t X3 9 B 3
@
cd L 4
S 0 F C + / 3 8 B O3
+ E L 4 Q/
F , 5 MF + / V 4 5 = L 3 . F 3 . C
L4n @ >
8 X - +E 3>3
@
3 3
@ >
L 4 Q/ 5 X .
,
0
3
S
@
+ - 3 +d
F3 BV>
S
L 4 . 3 - 3 BV 3
F
3. C
: + 3 F
/B. :/ . 4
3
0 ] F ,
4>
2Z Q ; 3
+/ L 4
3 3X zL
L 4 ^ 0 ^9
. F
3 03 3 > 3
.
X . F V
:4
0 F C + / 3 8 = c λ1=3
F - = c >
S
L4
:
JD 6 YD λ1=3 + 3 ^9
λ=6 10 + 3
(Z/R=1)
S
@
2Z
S
L4
Q; 3
. F3
9>3
` @ λ2 = 6
/
-
2
3
343
VW = 0/26
7D
L4
1D XZ
Blockage ratio
Turbulent mixing
L4
5/ ( ?P Q 7/ 7 *) 1 V4
- / '()
4 + -4 N
* / * 0 * .1 ' /
@
C
:
JD
(Z/R=1) 2Z
` @ λ 3 =10
@
3 03 ` @
/ 1D $ , / +,- MZ /-
4 + -3 N
X3 9 u ? 3
= 9 7C 3
S
c 5 = L 3 .
8 9
+ E 3 F 7C X3 9 = c . C
5 MF
-V 1
S
L4
Q;
B0 . 8
, €D >
6 + /X F) F
3>3 0 ] L 4.
F
\L 3
3
5 MF €t V B V 3 l 3
+ / L 4 R @> 3 .(8
X
? L ^JD
R` + 3. 4 ^ 4 L 4.
3 03y
L4
-0 4
* )O @ D ^_ U4)O
4 ;1
-
D9 €D > .
[20] *) 1 V4
/
@
3
VW = 0/54
. F3
-0 4
/ 5D $ , / +,- MZ /5/ ( ?P Q 7/ 7 *) 1 V4
- / '()
4 + -5 N
* / * 0 * .1 ' /
3 7 [20] > / (5 4) + /X F
F
.- U
.
75 q 3 +0 4R 0
V
3 > 3 + / +0 4R
2x X@ + 3 k − ω SST 5 MF R . 4
KA Z
@
4E
F > + /R 24 I . 4 F M 4 fE
X
B 3. C.
[20] > / +0 4 F . 4 . 2 23
1
q;
F 0 5 = L 3 . 4 F X@
+ 3 a b =1
0 I J >
4E
F I > 0 . 4 F X@ t
1
Viscous sublayer
343
3 >3
4>
λ1 = 3
=
r
-3
+/ L 4 3 = M
.
4
. D -2-4
4 3
K
3
L 4 +/
3 +d 0 -O3 3 > 3 . 4
8 9 IJ
λ2=6
Q/ . C + 4
L 4 5 = L 3.
v)C
p
+ D3 4 3 . 3
Q ; + :L
?L + 4
> 3 QV 1 7C AtV
3>3
4>
+ 0
L4
0 F + 8Y4 + /
9X F. V1
3
3
0]
0
F + 8Y4
λ1=3 + 3 3 X
+
L 4X
D -6 N
0 ] 1D
3>3
5) :M . '() N ,7)
4 + -7 N
e2=6 5-)* / * N .1 5/7 7 - ] 1D 7 / *
@
5) : M . '() N ,7)
4 + –8 N
e3 =10 5-)* / * N .1 5/7 7 - ] 1D 7 / * 0 * .1
wO- + 3
. DDE 0 + 3 0
+/
@ > 3 ; : 3 9 . 1 F 3 : m4
3 8 .
^9
. F 3 : I9 3 8 6 -V 1 + /
@ W2J F 3
wO- + 3 3 8 q O 4 ( 6 0 M 4
:/ i ? >
/( . /
./ 3 8 V4 .
R
.
. DDE Y4 / 3 8 .
wO- + 3 + 0 + /n 5
/ 3 8q O4
4 3 /( > > A I . 4 F 7 -
λ1 = 3
+ 3
^0 >
3. F
. 3
L4
X/D=0/62 X/D=- 0/62 0 λ2=6
Q;
L4Q; 3
QO 5 = L
3>3
- @
. C+ 4
L4
F
L4
L 4 . N2 O
+/ L 4
L4
λ1=3
4 -3(
+ 8 9 XE ) 3 > 3 ;
. C+ 4
L4 . 3
Q/
L4
+/
:4 3
@ 3
L 4>
F
/M
λ2 = 6
@ 3
4 -3
+/
8 9 XE
;
L4
= L 3. F
/- + : L 4
:4 3
3 . C 0 +d
F 3 .;
L4Q; 3 5
XE
;
L 4 Q/ > . 3
Q;
+/
: 9
C +/ 3 8
- B O3
> [:/ / S + 8 9
+ 3. C+ 5 > 4 >
:4 3
@ 3. F3 / 0 F
V
L 4 ^0
F „M@
L4
/
. F
/ * 0 * .1 -
-]
F
XZ
λ 2 =6 λ 1 =3
L4
+ 3 . C + 4
+ 8Y4
L 4 + / 3) /
Q : = M
4>
Q; 3
L4
/ .( 4 F ? . 3
0 F
Z/D=1 . 3
Q; . C+ 4
L4 4>
2Z
+ 3X/D= 0/52 X/D=- 0/52 XZ
. D
^0
M
0 * .1 - ]
A B . C +0 4
'()
3 >3
/ VW
3> 3
3 3 λ2 + 3
. F3
VW = 0/67
E
/
... + / L 4 3 D
=0/68 3 3 λ 3 + 3
-
5 6 *-/): -3-4
K 3 3>3
@
MF . C + / V 4 73 n7
+ /> 3
3 3 . C 0 XZ @
+/ 3 .
:
:/ 0 + 3 i ; @ B +0 4
73 > [:/
4>
3 +
8Q 3q @ i? > . 4
V3+ 3
n7 8o 6 .
@
MF + / V 4
^0
0 F C [
+/ 3 8 D E 3> 3 R @. C
4
344
>
10 X F)
@
6 . +C 3
. F
(v 10X F)
@
4
3-
M/ 3 3 λ 2 =6 + 3
wO- λ3 =10
L4
1 n/ 3 + / 3 8 0
@ 6
(N
/ 3 8W9
4
M4 (
3
3. F3
2f
L4.
8
4 3
∆ ([26]) g + / r
4 3
2E + / I
F
F C + / 3 8 10 X F . F 3 ([29]) gZ# ([28]) h ([27])
= M
+ / L 4 + KE L 4 .
3>3 0
F C +/ 3 8 I . /
. - gi ( 0 M 4 3
n
I M-
@ :E
I
4 4 3 3 λ1=3 + 3
(N )
(v)
"#$ / (' -
, O- [ *
5) :M . '() 5 6 -/)*)
4) 5
- / '()
5) :M . 5 6 . D -9 N
(b7/ . ) e2=6 (c) (I7- . )e1=3 (aP-) .(b. a4/ ) Z/D=7 7 (b7/ a4/ ) Z/D=4 (I7- a4/ ) Z/D=1 N$-., / X-Y
0
345
F C + / 3 8 = c λ1=3
0 F C+/ 3 8 F
L4
6 ;
. 3
@
Q;
7
Q; 3
0 F C +/ 3 8 ]
/
.- U >
L4Q; 3 5 = L 3. 3
Q;
L4
QV 1 = 9
@
3
Q/
, 3 8 > 3 2Z
345
3
5 V 0 F + / 3 + 3 + I . L 3 5 MF = F
11) + /X F . F
M 4 3 > 3 6 N2 O + /QO3
YV
N2 O XZ
5 MF = F
0 Y4 (13
F
. - N2 O
+/ L 4 + 3 3 X ;
D
- 3 8 = c λ3 =10
= c F
. F
-
. F
;
;
@
@ >
C +/ 3 8 3
L 4Q ; 3.
;
S 0
@
0 F C +/
F C+/ 3 8
... + / L 4 3 D
E
. 4
F
+ -3
0 F
0 F C+/ 3 8= c
A B . C +0 4
B
-4-4
3> 3
d # [9
(N )
(v)
(q)
e3 =10 (f) e2=6(c) e1=3 (aP-) a K
+ 3 L; 6
4>
3 + /> 3
@
n7
Z fV 6 . 4
- 7/ 5 6'()
mf K
V3+
/ 5- e"P '()
3 3> 3
3 :/ 0
-
/ / * 0 * .1 -
0 ] 5 MF = F 3
0 ] 5 MF = F I J
-
5 6 *-/): -10 N
3 X + 3
> 0. 4;1
5 MF = F
3 3>3
346
0 F C [
+/ 3 8 3 > 3 6 ;
4 F wO- . F
, > 3 + / QV 1 Y4
. F 3 / (0
;
n7 ^
/ 3 8
C + / 3 8 / . - 2E
- 3 € D (13 11) + /X F
€D > = c 4 >
2Z Q ; 3 F 3
0 F
U . F
-3
0 F C +/ 3 8 ,
-3
/ 3 8> = c l3
+/ L 4
/
.-
>
F3
n
I M-
@ :E
>
-]
5) :M .
d # [9
.
>3 0
0 F C + / 3 8 = c λ 1 =3
0 F C +/ 3 8 = c
8 , .
> 3 3. F :
+ 3. 3
Q ; 3 > 3 +/
L4Q; 3
L 4 (Z/R=1) 2Z
3X
? IIJD
R`
4 + -12 N
X9 @ λ3 =10
e2=6 5-)* / * N .1 5/7 7 - ] 1D 7 / * 0 * .1
D
` @
λ2 + 3 3 > 3
5 MF = F. F 3
S
-]
5) :M .
d # [9
e3 =10 5-)* / * N .1 5/7 7 - ] 1D 7 / * 0 * .1
-
. F3
TI=%11/01
5 MF = F
7D
1D XZ
@
TI=%19/98 3 3 λ3 + 3
P 3
4>
D
5 MF = F
TI=%14/62 3 3
2Z Q ; 3 -V 1 = 9
-5
- L 4 E D E 3>3 6 R @. C I J >
0 M 4 3 H ;3 + / 3 8 +0 4 F ( 3 = M
+/
. 4
8 9 IJ
4 3
8 :4
F 0R
+ L I J
/ 5- 0 U 3 3 V W3 J I J > U
->
L 4.
+
Fp, +/ 4 3.
> /
+ / L 4 Q ; + E L 4 Q/ 0
@ 3>3
4
. F3
C
.
4>
7C
3 > 3 0 > 8 2Z 3 C > 3
3. F
3 03
+/ L 4 :
>3
L4
S + 8 9 XE
L 4 : €D
L4Q;
-]
5) :M .
d # [9
4 + -11 N
e1=3 5-)* / * N .1 5/7 7 - ] 1D 7 / * 0 * .1
λ1=3 0 P 3 /
:
i? >
F ,
€D > = F
L4 Q; 3
4 • . F . F
€t V
5 MF = F Q ;
7C 3
8
-3 :
3 5 = L 3. F
^ 4
3 03y . C.
-3
+
2Z
L4 .
L4 Q;
L4.
: €D C . F
3 03 > 3
4>
S 0 F C+/ 3 8 = c BV 3
S XE
i 3 C 3. C.
+/
@ , ^9
. F3
1
347
@
5 MF = F X9 @ λ2=6
I B0 F i ? > . 3
Q ; λ3 =10
L 4+ 3
5 MF = F F MF . C
0 . 4 MF . C
@6
4 F , + /QV 1 = F - P 0 F
MF . C
1 . 3 Q ; 5 MF
R I
1
75 V
3 > [:/ . F I
3 At
I . 4
= F .;
8 wO- (13 11) + /X F 3 3
5
3 L4 1/ . 3
Q;
L 4 Q ; 3 5 MF
4 I B
= c A)@ B V 3
V
:4
. 4 /. C 5
I B
Q ; 5 MF = F
4 + -13 N
5) :
@ 0
4 TI=%6/12
Self-sustaining
347
/= 0/68
3 3
L 4 + /.
` @ 4 3 3
/ VW =0/26 3 3λ + 3
/ VW =0/54
L4
` @
L4Q; 3
1. 8
, i ? > F3
. 3
Q ; ; /. ]
F C+/ 3 8 I
Q; ;
L4 .
3 / 3 8 > c .;
7C > :/ 3
+/ L 4 > + 3 3 03 ` @
4
@ > . 3
λ2 + 3 /
VW = 0/67
3 3
.
: + r . 1 F 3 λ3+ 3 VW
.;
F C +/ 3 8 ]
I 1 8 5 = L 3
L 4.
3 03
9+ C c E
L 4.
3 F C +/ 3 8 ]
I
B0 .
1 c
. C.
5 MF = F . ^ B 3 . C .
€t V = F
U
5 MF = F 4 3 3 i ? > .
7C X3 9 c ;
. 3
Q ; 5 MF = F
/
. - ? @ I J 0 XZ @
3 S + 8 9 XE
2E
- 3€D +
5 MF = F
F
A B . C +0 4
L4+ 3
3> 3
λ2
3 8 XE QV 1
BV 3i ? >
E
. F 3 )8 c . C Y4 .
3
. F3 / 0 F C +/ 3 8 m
... + / L 4 3 D
[9] AubrunS., LoyerS., Hancock P.E., Hayden P.,Wind turbine
wake properties: Comparison between a non-rotating simplified
wind turbine model and a rotating model, J. Wind Eng. Ind.
AerodynVol.120, No. 1, pp. 1-8, 2013.
[10] Hu H., Yang Z., and Sarkar P., Dynamic wind loads and wake
characteristics of a wind turbine model in an atmospheric boundary
layer wind, Exp. Fluids, Vol. 52, No. 5, pp. 1277–1294, 2012.
[11] Zhang W., Markfort C. D., and Porté-Agel F., Near-wake flow
structure downwind of a wind turbine in a turbulent boundary layer,
Exp. Fluids, vol. 52, No. 5, pp. 1219–1235, 2012.
[12] Maeda T., Kamada Y., Murata J., Yonekura S., Ito T., Oawa
A. and Kogaki T.,Wind Tunnel Study on Wind and Turbulence
Intensity Profiles in Wind Turbine Wake, Journal of Thermal
Science Vol.20, No.2, pp.127-32, 2011
[13] Pope S., Turbulent flows, Cambridge University Press; 2000
[14] SmagorinskyJ., General circulation experiments with the
primitive equations: I. The basic equations, Monthly Weather
Review, Vol. 91, No. 3, pp. 99-164, 1963.
[15] GermanoM.,PiomelliU., MoinP., Cabot W. H., A dynamic
subgrid scale eddy viscosity model, Physics of Fluids A: Fluid
Dynamics, Vol. 3, No. 7, pp. 1760-1765, 1991.
[16] Lilly D. K., A proposed modification of the Germanosubgridscale closure method, Physics of Fluids A: Fluid Dynamics, Vol. 4,
No. 3, pp. 633-635, 1992
[17] MeneveauC., Lund T. S., and Cabot W. H., A Lagrangian
dynamicsubgrid-scale model of turbulence, Journalof Fluid
Mechanics, Vol. 319, No. 1, pp. 353-385, 1996
[18] BardinaJ., FerzigerJ. H., andReynolds W. C., Improved
subgrid models for large eddy simulation,13th Fluid and Plasma
Dynamics Conference, Stanford Univ.; CA, United States, July 1416, 1980
[19]Clark R. A., FerzigerJ. H. andReynolds W. C., Evaluation of
subgrid- scale models using an accurately simulated turbulent
flow,Journal of Fluid Mechanics, Vol. 91, No. 1, pp. 1-16, 1979
[20] KrogstadP. Å., Eriksen P. E., Blind test calculations of the
performance and wake development for a model wind turbine,
Renewable Energy, Vol. 50, No. C, pp. 325-333, 2013
[21]TanglerJ.L., Somers D. M., NREL airfoil families for
HAWTs,Proceedings of the American Wind Energy Association
Windpower Conference.Washington, National Renewable Energy
Laboratory; January 1995.
[22] Somers D., Design and experimental results for the S825
Airfoil, Technical Report NREL/SR-500-36344, National
Renewable Energy Laboratory, 1999.
[23]AlfredssonP. H., Dahlberg J. A., VermeulenP. E. J., A
comparison between predicted and measured data from wind
turbine wakes, Wind Engineering, Vol. 6, No. 3, pp. 149-155, 1982
[24] Medici D., AlfredssonP. H., Measurements on a wind turbine
wake: 3D Effects and bluff body vortex shedding, Wing Energy,
Vol. 9, No. 3, pp. 219-236, 2006
[25] SarmastS., Numerical study on instability and interaction of
wind turbine wakes, in Mechanics, Stability, Transition and
Control, PhD Thesis, KTH: Stockholm, 2013.
[26] Jeong, J., Hussain, F., On the identification of a vortex".
Journal of Fluid Mechanics, Vol. 285, No. 1, pp. 69-94, 1995
[27] Perry A. E., Chong M. E., and Cantwell B. J., "A general
classification of three-dimensional flow fields, Phys. Fluids A, Vol.
2, No. 5, pp. 765-777, 1990
[28] Hunt J. C. R., Wray A. A., and Moin P., Eddies, stream, and
convergence zones in turbulent flows, report ctr-s88. Center for
Turbulence Research, pages, pp. 193-208, 1988
[29] Zhou, J., Adrian R. J., Balachandar, S., and Kendall T. M.,
Mechanism for generating coherent packets of hairpin vortices in
channel flow, Journal of Fluid Mechanics, Vol. 387, No. 1, pp.
353-396, 1999
3 ^9
. F 3 λ1=3 0 P 3
+/ L 4 : 0
Q; > . C.
3 /. c
F C+/ 3 8 C
3
B0 .
C 3.
- 3€D ,
5 MF = F
- 3 8> = c F C+/ 3 8]
L 4Q ;
Q ; 3 7C > :/ 3 .
>30
>3
4>
/
X
Q ; (λ3 =100 P 3) 5 MF = F 4 >
> 3 0 2Z
+~
F C +/ 3 8 F X
3 5 = L 3 . 3
= F ,
L4 .
3 /. c > 3
4>
MF + /. C /
7C 3 i ? > . 3
Q ; 5 MF
.
/R I
- :/ 5 MF
.;
4
g -) -7
[1] Li Y., Paik K. J., Xing T., CarricaP. M. Dynamic overset CFD
simulations of wind turbine aerodynamics, renewable Energy, Vol.
52, No. 5, pp. 1219-1235, 2012.
[2] Zhang W., MarkfortC. D., Porte´-AgelF., Near-wake flow
structure downwind of a wind turbine in a turbulent boundary
layer,Experiments in Fluids,Vol. 52, No. 5, pp. 1219-1235, 2012.
[3]CrespoA., Hernandez J., FrandsenS., Survey of modeling
methods for wind turbine wakes and wind farms, Wind Energy,
Vol. 2, No. 1, pp. 1-24, 2012.
[4]Vermeer L.J., Sorensen J.N., CrespoA.; Wind turbine wake
aerodynamics;Progress in Aerospace Sciences,Vol. 39, No. 6-7, pp.
467-510, 2003.
[5] Mo. JO., ChoudhryA., ArjomandiM., Kelso R., Lee Y.
H.,Effects of wind speed changes on wake instability of a wind
turbine in a virtual wind tunnel using large eddy simulation,
Journal of Wind Engineering and Industrial Aerodynamic, Vol.
117, pp. 38-56, 2013.
[6]Porte, -AgelF., Wu Y. T., Lu H., ConzemiusR. J., Large-eddy
simulation of atmospheric boundary layer flow through wind
turbines and wind farms, Journal of Wind Engineering and
Industrial Aerodynamics, Vol. 99, No. 4, pp. 154-168, 2011.
[7] Stevens R. J. A. M.,GaymeD. F., MeneveauC., Large eddy
simulation studies of the effects of alignment and wind farm length,
Journal of Renewable and Sustainable Energy, Vol. 6, No. 2, pp.
611-623, 2014.
[8] Li Y., Paik K. J., Xing T., Carrica P. M., Dynamic overset CFD
simulations of wind turbine aerodynamics, renewable Energy
Vol.37, No. 1, pp. 285-298, 2012.
348
0
You can add this document to your study collection(s)
Sign in Available only to authorized usersYou can add this document to your saved list
Sign in Available only to authorized users(For complaints, use another form )